US9097798B2ActiveUtilityA1
Method for positioning determinations of receivers
Est. expiryApr 20, 2029(~2.8 yrs left)· nominal 20-yr term from priority
G01S 19/38G01S 19/48G01S 19/12
79
PatentIndex Score
7
Cited by
8
References
13
Claims
Abstract
The disclosed method and system is used to determine the position of a user device. The user device can receive data signals and/or carrier signals from orbiting space vehicles. These data signals can be used for positioning calculation and/or track maintenance of the user device. The disclosed method and system can account for time and frequency biases of the user device. For the track maintenance, a Kalman filter state estimator can be extended to include a velocity of the user device.
Claims
exact text as granted — not AI-modifiedWe claim:
1. A method for positioning calculations in an occluded environment comprising:
receiving signals from at least one space vehicle;
computing a pseudo range and a pseudo range rate including a time bias and a frequency bias of the signals; and
minimizing a cost function including the pseudo range and the pseudo range rate to obtain a position.
2. The method of claim 1 , wherein the cost function includes a product of the pseudo range and the pseudo range rate.
3. The method of claim 1 , wherein computing the pseudo range and the pseudo range rate includes a nonlinear least squares method.
4. The method of claim 1 , wherein computing the time bias and the frequency bias includes a linear least squares method.
5. The method of claim 1 , wherein the time bias and the frequency bias are expressed as explicit functions of a position of a user device.
6. The method of claim 1 , wherein expressions of the time bias and the frequency bias modify a cost function by removing the biases as independent states, thereby reducing the number of independent variables to those of a position of the user device alone.
7. The method of claim 1 , wherein the signal is received from a LEO satellite.
8. The method of claim 7 , wherein the LEO satellite is part of the Iridium system.
9. The method claim 1 , wherein the occluded environment includes at least one of an indoor environment, a jamming environment, and other environment where the signal is degraded by incidental or deliberate radio frequency interference.
10. The method of claim 1 , wherein obtaining the position of the user device is based on latitude and longitude information.
11. The method of claim 5 , wherein the user device comprises:
an antenna capable of receiving signals from at least one space vehicle; and
a computer system capable of processing the received signals to calculate a time bias and a frequency bias, the computer system using the time bias and the frequency bias to determine a position of the user device.
12. The method of claim 11 , wherein the computer system can execute an extended Kalman filter state estimator including a velocity of the user device in order to estimate a position of the user device if the antenna does not receive the signals of the at least on space vehicle.
13. The method of claim 11 , wherein the computer system further comprises an output device.Cited by (0)
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